TT-6645 GE FRAME 6B GAS TURBINE, YEAR 1981
TT-6645 GE FRAME 6B GAS TURBINE, YEAR 1981
1. 2X GE FRAME 6B GAS TURBINES
2. TECHNICAL SUMMARY
3. GAS TURBINES: TWO GE MS 6001 B GAS TURBINES PAIRED WITH AEG GENERATORS (TYPE S7102/2).
QUANTITY: 2
In stock
SKU
TT-6645
REFERENCE NUMBER: TT-6645
GE FRAME 6B GAS TURBINE, YEAR 1981
1. 2X GE FRAME 6B GAS TURBINES
2. TECHNICAL SUMMARY
3. GAS TURBINES: TWO GE MS 6001 B GAS TURBINES PAIRED WITH AEG GENERATORS (TYPE S7102/2).
4. OPERATION HISTORY:
5. YEAR COMMISSIONING: 1981
6. GAS-FIRED OPERATION: UNTIL 2005, PRIMARILY FOR BASE LOAD (~7000 HOURS/YEAR).
7. OPERATIONAL HOURS IN COMBINED CYCLE:
8. GT21: ~167,000 HOURS, ~1130 STARTS
9. GT22: ~159,000 HOURS, ~1180 STARTS
10. RETROFITTED: IN 1996 WITH WATER INJECTION FOR NOX REDUCTION.
11. CONVERSION: IN 2007 TO PEAK LOAD OPERATION USING HEATING OIL (HEL) WITH NEW STEEL CHIMNEYS AND UPGRADED CONTROL SYSTEMS TO ABB PROCONTROL 14.
12. OPERATIONAL HOURS IN PEAK LOAD:
13. GT21: ~130 HOURS, ~177 STARTS
14. GT22: ~150 HOURS, ~180 STARTS
15. LAST NETWORK OPERATION: 2015
16. LAST OIL SERVICE:
17. GT21: OCTOBER 2015
18. GT22: SEPTEMBER 2016
19. LAST BORESCOPE INSPECTION: DECEMBER 2016
20. DEFECT: HEATING OIL TRANSFER LINE ISSUE IN 2017 HALTED OPERATIONS.
21. DECOMMISSIONING: SEPTEMBER 2023
TECHNICAL SPECIFICATIONS
1. APPLICATION: GENERATOR DRIVE
2. SHAFT SPEED: 5105 RPM
3. CONTROL SYSTEM: ABB PROCONTROL 14
4. PROTECTION SYSTEMS: OVERSPEED, OVERTEMPERATURE, VIBRATION, AND FLAME MONITORING
5. COOLING MECHANISM: INTEGRATED ROTATION DEVICE IN THE TORQUE CONVERTER
ENVIRONMENTAL CONDITIONS
1. AMBIENT TEMPERATURE: 15°C
2. AIR PRESSURE: 0.9945 BAR
3. PRESSURE DROP IN INTAKE SYSTEM: 10.0 MBAR
4. EXHAUST DIFFUSER OUTLET PRESSURE: 30.0 MBAR
5. RELATIVE HUMIDITY: 60%
COMPRESSOR SECTION
1. STAGES: 17 AXIAL STAGES
2. TYPE: HIGH-PERFORMANCE AXIAL COMPRESSOR
3. CASING: HORIZONTALLY SPLIT
4. INLET GUIDE VANES: ADJUSTABLE
TURBINE SECTION
1. STAGES: 3 CONTINUOUS SHAFT STAGES
2. CASING: HORIZONTALLY SPLIT
3. GUIDE VANES: FIXED
COMBUSTION SYSTEM
1. TYPE: 10 CONCENTRIC RING CHAMBERS AROUND THE COMPRESSOR
2. FUEL NOZZLES: ONE PER CHAMBER, PRESSURE ATOMIZED
3. IGNITION: 2 SPRING-LOADED, SELF-RETRACTING ELECTRODE-TYPE SPARK PLUGS
4. FLAME MONITORS: 2 ULTRAVIOLET
BEARING ARRANGEMENT
1. NUMBER: 2
2. LUBRICATION:
3. BEARING NO. 1: PRESSURE LUBRICATED, COMBINATION OF THRUST AND JOURNAL BEARINGS
4. BEARING NO. 2: LEMON BORE JOURNAL BEARING
STARTING SYSTEM
1. DEVICE: DIESEL ENGINE (12 V-71-NT TURBOCHARGER)
2. TORQUE CONVERTER: HYDRAULIC WITH INTEGRATED REVERSING GEAR AND ROTATION DEVICE
FUEL SYSTEM
1. OPERATING FUEL: HEATING OIL (HEL)
2. FUEL PUMP: AUXILIARY GEAR-DRIVEN SCREW PUMP WITH CONSTANT FLOW
3. FUEL DISTRIBUTOR: FREE-ROTATING, 10 ELEMENTS
4. FUEL SHUTOFF VALVE: ELECTROHYDRAULIC SERVO CONTROL
5. FUEL FILTERS: 2 LOW-PRESSURE FULL-FLOW, 1 HIGH-PRESSURE FULL-FLOW
LUBRICATION SYSTEM
1. LUBRICANT: PETROLEUM-BASED
2. TOTAL VOLUME: ~7000 LITERS
3. MAIN OIL PUMP: SHAFT-DRIVEN, FLANGE-MOUNTED TO AUXILIARY GEARBOX
4. AUXILIARY AND EMERGENCY OIL PUMPS: MOTOR-DRIVEN SUBMERSIBLE CENTRIFUGAL PUMPS
HEAT EXCHANGER
1. TYPE: OIL/WATER
2. QUANTITY: SINGLE UNIT
LUBRICATION FILTERS
1. TYPE: FULL-FLOW WITH CHANGEOVER VALVE
2. QUANTITY: 2
3. FILTER TYPE: 5-MICRON
HYDRAULIC SYSTEM
1. PUMP: GEAR-DRIVEN AXIAL PISTON PUMP
2. FILTERS: 2 FULL-FLOW WITH CHANGEOVER VALVE
COOLING SYSTEM
1. PUMP: GEAR-DRIVEN CENTRIFUGAL PUMP
ATOMIZATION AIR SYSTEM
1. MAIN COMPRESSOR: GEAR-DRIVEN CENTRIFUGAL COMPRESSOR
2. STARTING COMPRESSOR: POSITIVE DISPLACEMENT PUMP DRIVEN BY STARTING DIESEL
3. PRE-COOLER: TUBULAR AND AIR/WATER HEAT EXCHANGER
4. AIR FILTER: CENTRIFUGAL SEPARATOR
PERFORMANCE DATA
1. OUTPUT AT GENERATOR TERMINALS (HEATING OIL): BASE LOAD 33.75 MW
2. EFFICIENCY: 29.9%
3. EXHAUST MASS FLOW: ~131.3 KG/S
4. EXHAUST TEMPERATURE: ~530°C
THE SPARE PARTS ARE:
1. COMPRESSOR AND TURBINE BLADING, USED (VARIOUS) AND REVISED (LEADING ROW 2 + 3 AND RUNNING ROW 1 + 2)
2. TRANSITION PIECES USED AND REVISED
3. FLAMMROHRE USED AND REVISED
4. FUEL NOZZLES AND MUCH MORE.
5. COVER SEGMENTS (NEW)
6. AS WELL AS A COMPLETE WAREHOUSE WITH SMALL PARTS (HYDRAULIC COMPONENTS, SCREW CONNECTIONS, SEALS, MEASUREMENT TECHNOLOGY, ETC.)
7. BRAND: GE
8. MODEL: FRAME 6B GAS TURBINE
9. YEAR: 1981
10. CONDITION: USED
QUANTITY: 2
Write Your Own Review